FMA I.A.50 Guarani II

1963

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FMA I.A.50 Guarani II

The Guarani I light transport first flew in prototype form on 6 February 1962 and utilised about 20% of the structural components of the IA.35 Huanquero. Power was provided by two 633kW Turbomeca Bastan IIIA turboprop engines. The Guarani II was developed from it and the prototype flew for the first time on 23 April 1963. It was placed in production for the Argentinian Air Force for communications, photographic (with the Military Geographic Institute) and executive transport duties, while the Navy received one as a staff transport. A total of 41 G.IIs were built.

FMA I.A.50 Guarani II

Specification 
 CREW1
 PASSENGERS10-15
 ENGINE2 x turbo-prop Turb. "Bastan IVA"
 WEIGHTS
  Take-off weight6500 kg14330 lb
  Empty weight4000 kg8819 lb
 DIMENSIONS
  Wingspan19.6 m64 ft 4 in
  Length15.3 m50 ft 2 in
  Height5.6 m18 ft 4 in
  Wing area41.8 m2449.93 sq ft
 PERFORMANCE
  Max. speed490 km/h304 mph
  Cruise speed485 km/h301 mph
  Ceiling3100 m10150 ft
  Range w/max.fuel2500 km1553 miles
  Range w/max payload2000 km1243 miles

Comments
THEBATTLEMASTER, 13.12.2012 22:22

Another odd looking plane made by FMA.

reply

marry, 18.06.2011 10:32

The IA50 GII makes regular commercial flights at Lineas Aereas Entre Rios (LAER)(Registration: LV-LAE and LV-LAI)

reply

Noname, e-mail, 31.03.2020 10:24

with the Military Geographic Institute

reply

Ariel G. San Martin, e-mail, 29.09.2010 04:07

The IA50 GII makes regular commercial flights at Lineas Aereas Entre Rios (LAER)(Registration: LV-LAE and LV-LAI)

reply

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